3:34ullQ3.pdfQ1) Air at mach number 2 , pressure 0.5* 10° N/m² and a temperature of 0 °C ,over a wedge and generation of an oblique shock wave 40° . determine :1. Static pressure and temperature downstream the shock.2. The mach number of the flow downstream the shock.3. The wedge angle.***********Q2) As shown in figure (1) A mach number 2.4 air stream at oblique shock angle of(B1-2 =30°) of incident shock with turning angle (0=10°). determine :1. the mach number of the flow upstream the reflected shock.2. the mach number of the flow downstream the reflected shock.M2M3Figure (1)

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Q1) Air at mach number 2 over a wedge and generation of an oblique shock wave 40° . determine : 1. Static pressure and temperature downstream the shock. 2. The mach number of the flow downstream the shock. , pressure 0.5* 10 N/m² and a temperature of 0 °C , 3. The wedge angle. ********* ********* ******** ***********************

Q1) Air at mach number 2 over a wedge and generation of an oblique shock wave 40° . determine : 1. Static pressure and temperature downstream the shock. 2. The mach number of the flow downstream the shock. , pressure 0.5* 10 N/m² and a temperature of 0 °C , 3. The wedge angle. ***** * *******************

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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